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Christophe Louembet
Christophe Louembet
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Adresse e-mail validée de laas.fr
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Designing continuously constrained spacecraft relative trajectories for proximity operations
G Deaconu, C Louembet, A Théron
Journal of Guidance, Control, and Dynamics 38 (7), 1208-1217, 2015
472015
Motion planning for flat systems using positive B-splines: An LMI approach
C Louembet, F Cazaurang, A Zolghadri
Automatica 46 (8), 1305-1309, 2010
432010
Robust rendezvous planning under maneuver execution errors
C Louembet, D Arzelier, G Deaconu
Journal of Guidance, Control, and Dynamics 38 (1), 76-93, 2015
412015
A new mixed iterative algorithm to solve the fuel-optimal linear impulsive rendezvous problem
D Arzelier, C Louembet, A Rondepierre, M Kara-Zaitri
Journal of Optimization Theory and Applications 159, 210-230, 2013
362013
A hybrid control framework for impulsive control of satellite rendezvous
M Brentari, S Urbina, D Arzelier, C Louembet, L Zaccarian
IEEE Transactions on Control Systems Technology 27 (4), 1537-1551, 2018
352018
Path planning for satellite slew manoeuvres: a combined flatness and collocation-based approach
C Louembet, F Cazaurang, A Zolghadri, C Charbonnel, C Pittet
IET control theory & applications 3 (4), 481-491, 2009
342009
Design of algorithms for satellite slew manoeuver by flatness and collocation
C Louembet, F Cazaurang, A Zolghadri, C Charbonnel, C Pittet
2007 American Control Conference, 3168-3173, 2007
342007
Minimizing the effects of navigation uncertainties on the spacecraft rendezvous precision
G Deaconu, C Louembet, A Théron
Journal of Guidance, Control, and Dynamics 37 (2), 695-700, 2014
282014
Using polynomial optimization to solve the fuel-optimal linear impulsive rendezvous problem
D Arzelier, M Kara-Zaitri, C Louembet, A Delibasi
Journal of Guidance, Control, and Dynamics 34 (5), 1567-1576, 2011
282011
A flatness-based predictive controller for six-degrees of freedom spacecraft rendezvous
JC Sanchez, F Gavilan, R Vazquez, C Louembet
Acta Astronautica 167, 391-403, 2020
262020
Model predictive control for rendezvous hovering phases based on a novel description of constrained trajectories
PRA Gilz, M Joldes, C Louembet, F Camps
IFAC-PapersOnLine 50 (1), 7229-7234, 2017
252017
Constrained periodic spacecraft relative motion using non-negative polynomials
G Deaconu, C Louembet, A Théron
2012 American Control Conference (ACC), 6715-6720, 2012
252012
Optimal control for minimum-fuel geostationary station keeping of satellites equipped with electric propulsion
C Gazzino, D Arzelier, D Losa, C Louembet, C Pittet, L Cerri
IFAC-PapersOnLine 49 (17), 379-384, 2016
232016
Long-term electric-propulsion geostationary station-keeping via integer programming
C Gazzino, D Arzelier, C Louembet, L Cerri, C Pittet, D Losa
Journal of guidance, control, and dynamics 42 (5), 976-991, 2019
222019
V-bar and r-bar glideslope guidance algorithms for fixed-time rendezvous: A linear programming approach
Y Ariba, D Arzelier, LS Urbina, C Louembet
IFAC-PapersOnLine 49 (17), 385-390, 2016
222016
Stable model predictive strategy for rendezvous hovering phases allowing for control saturation
PR Arantes Gilz, M Joldes, C Louembet, F Camps
Journal of Guidance, Control, and Dynamics 42 (8), 1658-1675, 2019
212019
Integer programming for optimal control of geostationary station keeping of low-thrust satellites
C Gazzino, C Louembet, D Arzelier, N Jozefowiez, D Losa, C Pittet, ...
IFAC-PapersOnLine 50 (1), 8169-8174, 2017
182017
Linearized impulsive fixed-time fuel-optimal space rendezvous: A new numerical approach
D Arzelier, F Bréhard, N Deak, M Joldes, C Louembet, A Rondepierre, ...
IFAC-PapersOnLine 49 (17), 373-378, 2016
182016
A three-step decomposition method for solving the minimum-fuel geostationary station keeping of satellites equipped with electric propulsion
C Gazzino, D Arzelier, L Cerri, D Losa, C Louembet, C Pittet
Acta Astronautica 158, 12-22, 2019
172019
Collision avoidance in low thrust rendezvous guidance using flatness and positive B-splines
C Louembet, G Deaconu
Proceedings of the 2011 American Control Conference, 456-461, 2011
172011
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