Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Damiana Losa"'
Autor:
Damiana Losa, Luca Cerri, Christophe Louembet, Clément Gazzino, Christelle Pittet, Denis Arzelier
Publikováno v:
Journal of Guidance, Control, and Dynamics
Journal of Guidance, Control, and Dynamics, 2019, 42 (5), pp.1-16. ⟨10.2514/1.G003644⟩
Journal of Guidance, Control, and Dynamics, American Institute of Aeronautics and Astronautics, 2019, 42 (5), pp.1-16. ⟨10.2514/1.G003644⟩
Journal of Guidance, Control, and Dynamics, 2019, 42 (5), pp.1-16. ⟨10.2514/1.G003644⟩
Journal of Guidance, Control, and Dynamics, American Institute of Aeronautics and Astronautics, 2019, 42 (5), pp.1-16. ⟨10.2514/1.G003644⟩
International audience; The problem of the computation of correction maneuvers for the fuel-optimal long-term station-keeping within a predefined longitude and latitude window of a geostationary satellite equipped with electric propulsion is investig
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::260ed3cfe4ced5eed31ba2ab2b42a281
https://hal.laas.fr/hal-02053120
https://hal.laas.fr/hal-02053120
Autor:
Denis Arzelier, Christelle Pittet, Christophe Louembet, Luca Cerri, Damiana Losa, Clément Gazzino
Publikováno v:
Acta Astronautica
Acta Astronautica, Elsevier, 2019, 158, pp.12-22. ⟨10.1016/j.actaastro.2018.08.015⟩
Acta Astronautica, 2019, 158, pp.12-22. ⟨10.1016/j.actaastro.2018.08.015⟩
Acta Astronautica, Elsevier, 2019, 158, pp.12-22. ⟨10.1016/j.actaastro.2018.08.015⟩
Acta Astronautica, 2019, 158, pp.12-22. ⟨10.1016/j.actaastro.2018.08.015⟩
International audience; In this paper, a control scheme is elaborated in order to perform the station keeping of a geostationary satellite equipped with electric propulsion while minimizing the fuel consumption. The use of electric thrusters imposes
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9738fe640cbe3cd9000bd43a1174d4b4
https://hal.laas.fr/hal-01696455v2/document
https://hal.laas.fr/hal-01696455v2/document
Autor:
Samir Bennani, Robert Fonod, David Henry, Damiana Losa, Catherine Charbonnel, Eric Bornschlegl
Publikováno v:
Control Engineering Practice. 42:12-27
This paper deals with the design and validation of an active fault-tolerant control system to detect, isolate and accommodate a single thruster fault affecting the thruster-based propulsion system of an autonomous spacecraft. The proposed method cons
Autor:
Christophe Louembet, Luca Cerri, Denis Arzelier, Damiana Losa, Nicolas Jozefowiez, Clément Gazzino, Christelle Pittet
Publikováno v:
Proceedings of the 20th IFAC World Congress
IFAC World Congress
IFAC World Congress, Jul 2017, Toulouse, France. pp.8499-8504
IFAC World Congress
IFAC World Congress, Jul 2017, Toulouse, France. pp.8499-8504
International audience; In this paper, a control scheme is elaborated to perform the station keeping of a geostationary satellite equipped with electric propulsion. The use of electric thrusters imposes to take into account some additional mutually e
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e92fa1de932380ebfd0cc965b446beff
https://hal.laas.fr/hal-01416694
https://hal.laas.fr/hal-01416694
Autor:
Clément Gazzino, Denis Arzelier, Luca Cerri, Christophe Louembet, Damiana Losa, Christelle Pittet
Publikováno v:
26th International Symposium on Space Flight Dynamics (ISSFD 2017)
26th International Symposium on Space Flight Dynamics (ISSFD 2017), Jun 2017, Matsuyama, Japan. 6p
Transactions of the Japan Society for Aeronautical and Space Sciences
Transactions of the Japan Society for Aeronautical and Space Sciences, Japan Society for Aeronautical and Space Sciences (J-STAGE), 2018, ISTS Special Issue, 16 (7), pp.628-634. ⟨10.2322/tastj.16.628⟩
Transactions of the Japan Society for Aeronautical and Space Sciences, 2018, ISTS Special Issue, 16 (7), pp.628-634. ⟨10.2322/tastj.16.628⟩
26th International Symposium on Space Flight Dynamics (ISSFD 2017), Jun 2017, Matsuyama, Japan. 6p
Transactions of the Japan Society for Aeronautical and Space Sciences
Transactions of the Japan Society for Aeronautical and Space Sciences, Japan Society for Aeronautical and Space Sciences (J-STAGE), 2018, ISTS Special Issue, 16 (7), pp.628-634. ⟨10.2322/tastj.16.628⟩
Transactions of the Japan Society for Aeronautical and Space Sciences, 2018, ISTS Special Issue, 16 (7), pp.628-634. ⟨10.2322/tastj.16.628⟩
International audience; In this paper, a fuel optimal rendezvous problem is tackled in the Hill-Clohessy-Wiltshire framework with several operational constraints as bounds on the thrust, non linear non convex and disjunctive operational constraints (
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9180a61f85cd402062245f902598f1fd
https://hal.laas.fr/hal-01511019/file/ArticleISSFD.pdf
https://hal.laas.fr/hal-01511019/file/ArticleISSFD.pdf
Publikováno v:
IFAC Proceedings Volumes. 44:2084-2089
Mission concepts proposed to return Mars soil samples to Earth involve a critical rendezvous phase with a passive sample container placed in Mars orbit by an ascent vehicle. An innovative magnetic capture device was recently proposed to increase the
Publikováno v:
IFAC Proceedings Volumes. 44:1878-1882
European leader for satellite systems and at the forefront of orbital infrastructures, Thales Alenia Space is a joint venture between Thales (67%) and Finmeccanica (33%) and forms with Telespazio a Space Alliance. Thales Alenia Space is a worldwide r
Publikováno v:
Advances in Aerospace Guidance, Navigation and Control ISBN: 9783319175171
Employing only bearing/angular measurements for navigation during the far to medium range rendezvous with a non-cooperative target has several advantages with respect to directly measuring the range using active sensors such as RADAR or LIDAR. Angula
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::62b28a60abbd7e8d75d45cd4e67e9643
https://doi.org/10.1007/978-3-319-17518-8_33
https://doi.org/10.1007/978-3-319-17518-8_33
Publikováno v:
Advances in Aerospace Guidance, Navigation and Control ISBN: 9783642382529
In-orbit rendezvous is a key enabling technology for many space missions. Implementing it employing only bearing measurements would simplify the relative navigation hardware currently required, increasing robustness and reliability by reducing comple
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::27c2a5a4af062d0209e74dfbfd1f5adb
https://doi.org/10.1007/978-3-642-38253-6_14
https://doi.org/10.1007/978-3-642-38253-6_14