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Spilios Theodoulis
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2020 – today
- 2022
- [c13]Sofiane Pineau, Spilios Theodoulis, Michel Zasadzinski, Mohamed Boutayeb:
Autopilot Design for Dual-Spin Projectiles using Incremental Nonlinear Dynamic Inversion. MED 2022: 444-449 - 2021
- [c12]Sovanna Thai, Clément Roos, Jean-Marc Biannic, Spilios Theodoulis:
An Interpolated Model Recovery Anti-Windup for a Canard-Guided Projectile Subject to Uncertainties. ECC 2021: 1693-1698 - 2020
- [c11]Sovanna Thai, Spilios Theodoulis, Clément Roos, Jean-Marc Biannic, Michael Proff:
Gain-Scheduled Autopilot Design with Anti-Windup Compensator for a Dual-Spin Canard-Guided Projectile. CCTA 2020: 156-161 - [c10]Spilios Theodoulis, Michael Proff, Charlotte Marchand:
Robust Design for Highly Agile Missile Autopilots. MED 2020: 67-72
2010 – 2019
- 2017
- [j2]Florian Seve, Spilios Theodoulis, Philippe Wernert, Michel Zasadzinski, Mohamed Boutayeb:
Flight Dynamics Modeling of Dual-Spin Guided Projectiles. IEEE Trans. Aerosp. Electron. Syst. 53(4): 1625-1641 (2017) - [c9]Sebastian Fleischmann, Spilios Theodoulis, Edouard Laroche, Elmar Wallner, Jean-Philippe Harcaut:
Controller design point selection for linearized gain scheduling. ACC 2017: 1574-1579 - 2014
- [c8]Guillaume Strub, Vincent Gassmann, Spilios Theodoulis, Simona Dobre, Michel Basset:
Hardware-in-the-loop experimental setup development for a guided projectile in a wind tunnel. AIM 2014: 458-463 - [c7]Florian Seve, Spilios Theodoulis, Philippe Wernert, Michel Zasadzinski, Mohamed Boutayeb:
Sensor position influence on modeling and control of 155mm canard-guided spin-stabilized projectiles. CoDIT 2014: 358-363 - [c6]Florian Seve, Spilios Theodoulis, Michel Zasadzinski, Mohamed Boutayeb, Philippe Wernert:
Fixed structure ℋ∞ Control for a canard-guided projectile pitch/yaw dynamics autopilot design. ECC 2014: 594-599 - [c5]Leif Walter, Gunther Schloffel, Spilios Theodoulis, Philippe Wernert, Ekaterina A. Kostina, Florian Holzapfel
:
Optimal control and numerical optimization for missile interception guidance. ECC 2014: 1249-1255 - [c4]Florian Seve, Spilios Theodoulis, Michel Zasadzinski, Mohamed Boutayeb, Philippe Wernert:
Comparison of two H∞ loop-shaping robust autopilot structure configurations for a 155mm spin-stabilized canard-guided projectile. MED 2014: 1147-1152 - 2013
- [c3]Spilios Theodoulis, Vincent Gassmann, Thomas Brunner, Philippe Wernert:
Fixed structure robust control design for the 155mm canard-guided projectile roll-channel autopilot. MED 2013: 155-160 - 2011
- [j1]Spilios Theodoulis, Yannick Morel, Philippe Wernert:
Modelling and stability analysis of the 155 mm spin-stabilised projectile equipped with steering fins. Int. J. Model. Identif. Control. 14(3): 189-204 (2011)
2000 – 2009
- 2007
- [c2]Spilios Theodoulis, Gilles Duc:
Static interpolated ℋ∞ loop-shaping controllers for missile autopilot synthesis. CDC 2007: 2385-2392 - [c1]Mohamed Abbas-Turki, Gilles Duc, Benoit Clement
Robust gain scheduled control of a space launcher by introducing LQG/LTR ideas in the NCF robust stabilisation problem. CDC 2007: 2393-2398
Coauthor Index
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