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Spilios Theodoulis
Spilios Theodoulis
Associate Professor, TU Delft
Preverjeni e-poštni naslov na tudelft.nl - Domača stran
Naslov
Navedeno
Navedeno
Leto
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
1192013
Missile autopilot design: gain-scheduling and the gap metric
S Theodoulis, G Duc
Journal of guidance, control, and dynamics 32 (3), 986-996, 2009
852009
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
552015
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
452017
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
312011
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
282010
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
262020
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
262014
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
212009
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
202011
Flight dynamics & control for smart munition: the ISL contribution
S Theodoulis, P Wernert
IFAC-PapersOnLine 50 (1), 15512-15517, 2017
172017
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
172017
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
162019
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
162011
Robust flight control tuning for highly agile missiles
S Theodoulis, M Proff
Aiaa scitech 2021 forum, 1568, 2021
132021
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
132010
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
122015
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
122014
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
122012
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