Flight dynamics modeling of dual-spin guided projectiles

Autor: Philippe Wernert, Spilios Theodoulis, Florian Sève, Michel Zasadzinski, Mohamed Boutayeb

Publikováno v: IEEE Transactions on Aerospace and Electronic Systems
IEEE Transactions on Aerospace and Electronic Systems, Institute of Electrical and Electronics Engineers, 2017, 53 (4), pp.1625-1641. ⟨10.1109/TAES.2017.2667820⟩

International audience; This paper presents a complete nonlinear parameter-dependent mathematical model, as well as a procedure for computing the quasi-linear parameter-varying (q-LPV) model of a class of spin-stabilized canard-controlled guided proj

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5773ffa56bf8176c215e52c2e96dda25
https://hal.archives-ouvertes.fr/hal-01657860

Sensor position influence on modeling and control of 155mm canard-guided spin-stabilized projectiles

Autor: Florian Sève, Spilios Theodoulis, Philippe Wernert, Michel Zasadzinski, Mohamed Boutayeb

Publikováno v: CoDIT
International Conference on Control, Decision and Information Technologies, CoDIT'14
International Conference on Control, Decision and Information Technologies, CoDIT'14, Nov 2014, Metz, France

International audience; This article explores in detail the influence of the sensor position on the pitch/yaw dynamics modeling and on the autopilot design and performance for a 155mm canard-guided spin-stabilized projectile which incorporates a nose

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d88bca26f878480fda58295b54ba0e45
https://doi.org/10.1109/codit.2014.6996920

Comparison of two H∞ loop-shaping robust autopilot structure configurations for a 155mm spin-stabilized canard-guided projectile

Autor: Michel Zasadzinski, Spilios Theodoulis, Philippe Wernert, Mohamed Boutayeb, Florian Sève

Publikováno v: MED

This article deals with the design of a pitch/yaw dynamics load factor autopilot for a 155mm spin-stabilized projectile which is controlled using a nose-mounted course correction fuse equipped with two rotating aerodynamic surfaces. A q-LPV model nec

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::676723925d74d453480f4a480523329e
https://doi.org/10.1109/med.2014.6961530

Robust Bank-to-Turn Autopilot Design for a Class of 155mm Spin-Stabilized Canard-Guided Projectiles

Autor: Thomas Brunner, Spilios Theodoulis, Philippe Wernert, Vincent Gassmann

Publikováno v: AIAA Atmospheric Flight Mechanics (AFM) Conference.

This article details the design of a Bank-to-Turn autopilot for a class of 155mm spinstabilized ammunition which incorporates a nose-positioned course correction fuse used for trajectory correction and range extension. The considered concept aft sect

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::64c83174f0ae397163838366aa637f22
https://doi.org/10.2514/6.2013-4608

Flight Control for a Class of 155 mm Spin-stabilized Projectile with Reciprocating Canards

Autor: Julien Spagni, Spilios Theodoulis, Philippe Wernert

Publikováno v: AIAA Guidance, Navigation, and Control Conference.

This article presents a feasibility study for the design and analysis of a longitudinal/lateral axes autopilot for a class of reciprocating canard-guided artillery munitions. A realistic yet exploitable nonlinear mathematical model of the projectile

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::399760c68ca343af7c3b0106579ce092
https://doi.org/10.2514/6.2012-4685