| 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 | 117 | 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 | 84 | 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 | 51 | 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 | 40 | 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 |
| 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 | 26 | 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 | 25 | 2014 |
| 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 |
| 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 | 20 | 2020 |
| 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 |
| 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 |
| Gain-scheduled loop-shaping autopilot design for spin-stabilized canard-guided projectiles F Sève, S Theodoulis, P Wernert, M Zasadzinski, M Boutayeb Aerospace Lab, 1-24, 2017 | 15 | 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 | 14 | 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 | 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 |
| 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 | 12 | 2010 |
| Robust flight control tuning for highly agile missiles S Theodoulis, M Proff AIAA Scitech 2021 Forum, 1568, 2021 | 11 | 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 | 11* | 2019 |
| 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 | 11 | 2015 |
Mohamed BoutayebUniversité de LorraineVerifierad e-postadress på univ-lorraine.fr
