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
103 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
77 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
41 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
34 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
30 2011 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
22 2014 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
21 2010 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
20 2009 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
18 2020 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 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
15 2011 Gain-scheduled F Sève, S Theodoulis, P Wernert, M Zasadzinski, M Boutayeb
Aerospace Lab, 1-24, 2017
12 2017 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 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
11 2019 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
11 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
11 2012 Robust gain scheduled control of a space launcher by introducing LQG/LTR ideas in the NCF robust stabilisation problem M Abbas-Turki, G Duc, B Clement, S Theodoulis
2007 46th IEEE Conference on Decision and Control, 2393-2398, 2007
11 2007 Flight dynamics & control for smart munition: the ISL contribution S Theodoulis, P Wernert
IFAC-PapersOnLine 50 (1), 15512-15517, 2017
10 2017 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
10 2010 Pitch axis control for a guided projectile in a wind tunnel hardware-in-the-loop setup G Strub, S Theodoulis, V Gassmann, S Dobre, M Basset
Journal of Spacecraft and Rockets 52 (6), 1614-1626, 2015
9 2015 
Mohamed BoutayebUniversité de LorraineEmail verificata su univ-lorraine.fr
