Guidance and control design for a class of spin-stabilized fin-controlled projectiles S Theodoulis, V Gassmann, P Wernert, L Dritsas, I Kitsios, A Tzes
Journal of Guidance, Control, and Dynamics 36 (2), 517-531, 2013
119 2013 Missile autopilot design: gain-scheduling and the gap metric S Theodoulis, G Duc
Journal of guidance, control, and dynamics 32 (3), 986-996, 2009
85 2009 Robust gain-scheduled autopilot design for spin-stabilized projectiles with a course-correction fuze S Theodoulis, F Sève, P Wernert
Aerospace Science and Technology 42, 477-489, 2015
55 2015 Flight dynamics modeling of dual-spin guided projectiles F Seve, S Theodoulis, P Wernert, M Zasadzinski, M Boutayeb
IEEE Transactions on Aerospace and Electronic Systems 53 (4), 1625-1641, 2017
45 2017 Modelling and stability analysis for a class of 155 mm spin-stabilized projectiles with course correction fuse (CCF) P Wernert, S Theodoulis
AIAA atmospheric flight mechanics conference, 6269, 2011
31 2011 Flight dynamics properties of 155 mm spin-stabilized projectiles analyzed in different body frames P Wernert, S Theodoulis, Y Morel
AIAA atmospheric flight mechanics conference, 7640, 2010
28 2010 Pitch/yaw channels control design for a 155mm projectile with rotating canards, using a H∞ loop-shaping design procedure F Sève, S Theodoulis, P Wernert, M Zasadzinski, M Boutayeb
AIAA Guidance, Navigation, and Control Conference, 1474, 2014
26 2014 Nonlinear dynamic inversion flight control design for guided projectiles S Tipàn, S Theodoulis, S Thai, M Proff
Journal of Guidance, Control, and Dynamics 43 (5), 975-980, 2020
25 2020 Modeling and control of two GLMAV hover-flight concepts P Gnemmi, A Koehl, B Martinez, S Changey, S Theodoulis
Proceedings of the European micro aerial vehicle conference, 2009
21 2009 Flight control for a class of 155 mm spin-stabilized projectiles with course correction fuse (CCF) S Theodoulis, P Wernert
AIAA Guidance, Navigation, and Control Conference, 6247, 2011
20 2011 Flight dynamics & control for smart munition: the ISL contribution S Theodoulis, P Wernert
IFAC-PapersOnLine 50 (1), 15512-15517, 2017
17 2017 Gain-scheduled F Sève, S Theodoulis, P Wernert, M Zasadzinski, M Boutayeb
Aerospace Lab, 1-24, 2017
17 2017 Robust design for the roll-channel autopilot of a canard-guided dual-spin projectile S Thai, S Theodoulis, C Roos, JM Biannic
IFAC-PapersOnLine 52 (12), 232-237, 2019
16 2019 Modelling and stability analysis of the 155 mm spin-stabilised projectile equipped with steering fins S Theodoulis, Y Morel, P Wernert
International Journal of Modelling, Identification and Control 14 (3), 189-204, 2011
16 2011 Robust flight control tuning for highly agile missiles S Theodoulis, M Proff
Aiaa scitech 2021 forum, 1568, 2021
13 2021 Design of an Hinf Gain-Scheduled Guidance Scheme for a Guided Projectile FSS Theodoulis
Journal of Guidance, Control & Dynamics 42 (11), 2399-2417, 2019
13 * 2019 LPV modeling of guided projectiles for terminal guidance S Theodoulis, Y Morel, P Wernert, A Tzes
18th Mediterranean Conference on Control and Automation, MED'10, 1455-1460, 2010
13 2010 Pitch axis control for a guided projectile in a wind tunnel-based hardware-in-the-loop setup G Strub, S Theodoulis, V Gassmann, S Dobre, M Basset
AIAA Modeling and Simulation Technologies Conference, 0153, 2015
12 2015 Hardware-in-the-loop experimental setup development for a guided projectile in a wind tunnel G Strub, V Gassmann, S Theodoulis, S Dobre, M Basset
2014 IEEE/ASME International Conference on Advanced Intelligent Mechatronics …, 2014
12 2014 Flight control for a class of 155 mm spin-stabilized projectile with reciprocating canards J Spagni, S Theodoulis, P Wernert
AIAA Guidance, Navigation, and Control Conference, 4685, 2012
12 2012 
Mohamed BoutayebUniversité de LorraineEmail verificata su univ-lorraine.fr