Zobrazeno 1 - 10
of 14
pro vyhledávání: '"Marie Albisser"'
Publikováno v:
IFAC-PapersOnLine; January 2024, Vol. 58 Issue: 21 p208-213, 6p
Publikováno v:
AIAA Journal
AIAA Journal, American Institute of Aeronautics and Astronautics, 2020, 58 (7), pp.3139-3148. ⟨10.2514/1.J059065⟩
AIAA Journal, 2020, 58 (7), pp.3139-3148. ⟨10.2514/1.J059065⟩
AIAA Journal, American Institute of Aeronautics and Astronautics, 2020, 58 (7), pp.3139-3148. ⟨10.2514/1.J059065⟩
AIAA Journal, 2020, 58 (7), pp.3139-3148. ⟨10.2514/1.J059065⟩
International audience; A vehicle’s in-flight behavior can be represented by the Newton–Euler equations of motion: usually, such a model has a nonlinear and continuous description based on ordinary differential equations. The model structure can
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ff53727458ed5a3e98e70c80c3dcfc21
https://hal.archives-ouvertes.fr/hal-02892171
https://hal.archives-ouvertes.fr/hal-02892171
Autor:
Marie Albisser, Simona Dobre
Publikováno v:
IFAC-PapersOnLine. 51:963-968
The parameter identification of grey-box nonlinear model structures remains a challenging task. Analytical models, constructed from physical laws, allow a complete description of the system behavior, with however a high complexity of the mathematical
Publikováno v:
Journal of Spacecraft and Rockets
Journal of Spacecraft and Rockets, American Institute of Aeronautics and Astronautics, 2017, 54 (2), pp.426-435. ⟨10.2514/1.A33587⟩
Journal of Spacecraft and Rockets, American Institute of Aeronautics and Astronautics, 2017, 54 (2), pp.426-435. ⟨10.2514/1.A33587⟩
International audience; The identification of aerodynamic coefficients, based on free-flight measurements, remains complex and challenging for vehicles such as space probes, unmanned aerial vehicles, or ammunition. In this paper, a detailed procedure
Publikováno v:
Ninth International Conference on Sensitivity Analysis of Model Output, SAMO 2019
Ninth International Conference on Sensitivity Analysis of Model Output, SAMO 2019, Oct 2019, Barcelone, Spain
HAL
Ninth International Conference on Sensitivity Analysis of Model Output, SAMO 2019, Oct 2019, Barcelone, Spain
HAL
Présentation Poster; International audience
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::dd551323212613d4c00f673c9569a845
https://hal.archives-ouvertes.fr/hal-02386116
https://hal.archives-ouvertes.fr/hal-02386116
Publikováno v:
AIAA Scitech 2019 Forum
AIAA Scitech 2019 Forum, Jan 2019, San Diego, CA, United States. pp.1321, ⟨10.2514/6.2019-1321⟩
AIAA Scitech 2019 Forum, Jan 2019, San Diego, CA, United States. pp.1321, ⟨10.2514/6.2019-1321⟩
International audience; A vehicle's in-flight behaviour can be represented by the Newton-Euler equations of motion: usually, such a model has a nonlinear and continuous description based on ordinary differential equations. The model structure can be
Publikováno v:
18th IFAC Symposium on System Identification, SYSID 2018
18th IFAC Symposium on System Identification, SYSID 2018, Jul 2018, Stockholm, Sweden. ⟨10.1016/j.ifacol.2018.09.050⟩
18th IFAC Symposium on System Identification, SYSID 2018, Jul 2018, Stockholm, Sweden. ⟨10.1016/j.ifacol.2018.09.050⟩
Published in IFAC-PapersOnLine 51(15):1080-1085, 2018; International audience; The behaviour of a projectile in flight is usually described by the Newton-Euler equations of motion, through a nonlinear model structure. Its transformation into a quasi-
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5c8cf6ed8118da387bcc40fa41a2a82f
https://hal.archives-ouvertes.fr/hal-01918818
https://hal.archives-ouvertes.fr/hal-01918818
Autor:
Jean-Claude Roy, Marie Albisser, Yannick Bailly, Patrick Gnemmi, Cédric Decrocq, Simona Dobre, Bastien Martinez
Publikováno v:
International Journal of Numerical Methods for Heat and Fluid Flow
International Journal of Numerical Methods for Heat and Fluid Flow, Emerald, 2018, 28 (5), pp.1218-1236
International Journal of Numerical Methods for Heat and Fluid Flow, Emerald, 2018, 28 (5), pp.1218-1236
Purpose The present paper deals with weapon aerodynamics and aims to describe preliminary studies that were conducted for developing the next generation of long-range guided ammunition. Over history, ballistic research scientists were constantly inve
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4e1dbe44daa0c4561321c1c1b9c711ad
https://hal.archives-ouvertes.fr/hal-02370578
https://hal.archives-ouvertes.fr/hal-02370578
Publikováno v:
30th International Symposium on Ballistics.
This paper presents the aerodynamic characterization of a new concept of long range projectile, fitted with six fins. Three distinct projectile architectures were investigated: two with canted fins, while the last one presents twisted fins. The aerod
Publikováno v:
20th IFAC World Congress, IFAC 2017
20th IFAC World Congress, IFAC 2017, Jul 2017, Toulouse, France
HAL
20th IFAC World Congress, IFAC 2017, Jul 2017, Toulouse, France
HAL
International audience; Ballistic testing of flying vehicles, such as space probes or projectiles, is an important part of their design. The model describing the behaviour of a vehicle in free flight is nonlinear, characterised by the off-equilibrium
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::000683d2c325f9687eb1937641509f39
https://hal.archives-ouvertes.fr/hal-01567445
https://hal.archives-ouvertes.fr/hal-01567445