Zobrazeno 1 - 10
of 123
pro vyhledávání: '"Daniel Alazard"'
Publikováno v:
IEEE Transactions on Control Systems Technology. 31:418-425
This brief proposes a new linear fractional transformation (LFT) modeling approach for uncertain linear parameter-varying (LPV) multibody systems with parameter-dependent equilibrium. Traditional multibody approaches, which consist of building the no
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::fe267c6cbb110612c00df41b4846a089
https://doi.org/10.1109/tcst.2022.3167610
https://doi.org/10.1109/tcst.2022.3167610
Publikováno v:
Multibody System Dynamics.
In the context of multi-body modeling techniques, this paper details the port inversion operations, which can be performed on the Two-Input-Two-Output Port (TITOP) model of a flexible substructure to take into account various boundary conditions and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::21ee2af64857a7f63ee5662af5026ed5
https://oatao.univ-toulouse.fr/29501/
https://oatao.univ-toulouse.fr/29501/
Autor:
Francesco Pace, Emanuele Paolini, Francesco Sanfedino, Daniel Alazard, Andrea Colagrossi, Vincenzo Pesce, Stefano Silvestrini
Publikováno v:
Modern Spacecraft Guidance, Navigation, and Control ISBN: 9780323909167
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::098904c9a312adbbe3cbe1a7f67bfe3e
https://doi.org/10.1016/b978-0-323-90916-7.00012-3
https://doi.org/10.1016/b978-0-323-90916-7.00012-3
Autor:
Stefano Silvestrini, Andrea Colagrossi, Emanuele Paolini, Aureliano Rivolta, Andrea Capannolo, Vincenzo Pesce, Shyam Bhaskaran, Francesco Sanfedino, Daniel Alazard
Publikováno v:
Modern Spacecraft Guidance, Navigation, and Control ISBN: 9780323909167
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::00f57135da09960dd871b7bd02b7ff6c
https://doi.org/10.1016/b978-0-323-90916-7.00014-7
https://doi.org/10.1016/b978-0-323-90916-7.00014-7
Autor:
Daniel Alazard, Matteo Battilana, Shyam Bhaskaran, Andrea Capannolo, Lorenzo Pasqualetto Cassinis, Francesco Cavenago, Andrea Colagrossi, Filippo Corradino, David Gonzalez-Arjona, Pablo Hermosin, Robert Hinz, Francesco Pace, Emanuele Paolini, Vincenzo Pesce, Thomas Peters, Aureliano Rivolta, Francesco Sanfedino, Stefano Silvestrini, Massimo Tipaldi, Pierluigi Visconti, Lisa Whittle
Publikováno v:
Modern Spacecraft Guidance, Navigation, and Control ISBN: 9780323909167
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::63d53aaec3cb8ee684c6a6cdd4f00b5f
https://doi.org/10.1016/b978-0-323-90916-7.01002-7
https://doi.org/10.1016/b978-0-323-90916-7.01002-7
Autor:
Daniel Alazard, Valérie Pommier-Budinger, Samir Bennani, Francesco Sanfedino, Valentin Preda, Fabrice Boquet
Publikováno v:
IEEE Transactions on Control Systems Technology
IEEE Transactions on Control Systems Technology, Institute of Electrical and Electronics Engineers, 2020, pp.1-16. ⟨10.1109/TCST.2020.2970658⟩
IEEE Transactions on Control Systems Technology, Institute of Electrical and Electronics Engineers, 2020, pp.1-16. ⟨10.1109/TCST.2020.2970658⟩
International audience; Modern space-observation missions demand stringent pointing requirements that motivated a significant amount of research on the topic of microvibration isolation and line-of-sight stabilization systems. While disturbances can
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::707ad524eb896b4967d4be5a886fce24
https://doi.org/10.1109/tcst.2020.2970658
https://doi.org/10.1109/tcst.2020.2970658
Autor:
Louis Dubois, Hélène Evain, Ismael Vivo-Martin, Francesco Sanfedino, Daniel Alazard, Mathieu Rognant, Gabriel Galvao-Adarme, Ervan Kassarian, Corentin Chauffaut
Publikováno v:
IFAC-PapersOnLine. 54:61-67
This paper presents the development of an Extended Kalman Filter for the navigation system of a spacecraft in a parabolic flight. The algorithm blends the measurements coming from two Inertia Measurement Units, one mounted on the spacecraft and one o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f644bdaa0e4b17194797044ef5653134
https://doi.org/10.1016/j.ifacol.2021.11.017
https://doi.org/10.1016/j.ifacol.2021.11.017
Publikováno v:
CEAS Aeronautical Journal
CEAS Aeronautical Journal, Springer, 2020, ⟨10.1007/s13272-020-00481-8⟩
CEAS Aeronautical Journal, Springer, 2020, ⟨10.1007/s13272-020-00481-8⟩
A sequential co-design framework has been developed in a previous study (Nguyen-Van et al., IFAC-PapersOnLine 52(12):514–519, https://doi.org/10.1016/j.ifacol.2019.11.295 , 2019)) to design an aircraft using active differential thrust. Differential
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2fda02b2be423178a3c799d0208592d6
https://doi.org/10.1007/s13272-020-00481-8
https://doi.org/10.1007/s13272-020-00481-8
Publikováno v:
IFAC-PapersOnLine. 53:14851-14856
This paper addresses the issue of controlling a spacecraft with a redundant pyramidal Control Moment Gyro (CMG) cluster. A rapid analysis of the mathematical problem to steer the attitude control system is carried out with a focus on how to use the r
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8692156970d7f72643877a4da7a6c384
https://doi.org/10.1016/j.ifacol.2020.12.1932
https://doi.org/10.1016/j.ifacol.2020.12.1932
Publikováno v:
AIAA SCITECH 2022 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a6761dc3da4093e3635222fe66c56676
https://doi.org/10.2514/6.2022-2243.c1
https://doi.org/10.2514/6.2022-2243.c1