Zobrazeno 1 - 10
of 34
pro vyhledávání: '"Luis F. Peñín"'
Autor:
Jose A. Ospina, Victor Marco, Rafael Contreras, Elio Zaccagnino, Gabriale De Zaiacomo, Daniel Serrano, Jean-Philippe Preaud, Juan Antonio Bejar-Romero, Ricardo Yague, Murray Kerr, Guillermo Rodriguez, Rodrigo Haya-Ramos, Raul Sanchez, Luis F. Peñín, Vicente Fernández
Publikováno v:
Acta Astronautica. 124:53-66
The Intermediate eXperimental Vehicle (IXV) [1] is an ESA re-entry lifting body demonstrator built to verify in-flight the performance of critical re-entry technologies. The IXV was launched on February the 11th, 2015, aboard Europe's Vega launcher.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::10e8eac7830900fb8f0cda75def0376d
https://doi.org/10.1016/j.actaastro.2016.04.010
https://doi.org/10.1016/j.actaastro.2016.04.010
Autor:
J. C. Bastante, José F. Vasconcelos, João Dinis, José Manuel Rebordão, Luis F. Peñín, Miguel Hagenfeldt
Publikováno v:
Acta Astronautica. 102:311-320
PROBA-3 is a technology demonstration mission with the objective of, among others, raising the Formation Flying (FF) technology up to Technology Readiness Level (TRL) 8 or 9. The context of this mission has strong synergies with the knowledge areas c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::39c8fa54c4a5b6654acd04c44c10bbd6
https://doi.org/10.1016/j.actaastro.2013.11.018
https://doi.org/10.1016/j.actaastro.2013.11.018
Publikováno v:
Scopus-Elsevier
In this article a fault detection and isolation scheme based on H ∞ theory is presented for a rocket engine actuator valve. The simulation model of the engine corresponds to a Vulcain 2-like rocket engine used to study the applicability and capabil
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4e11aa6b1339e8233ced5ed3bfeed129
https://doi.org/10.3182/20130902-5-de-2040.00048
https://doi.org/10.3182/20130902-5-de-2040.00048
Publikováno v:
Scopus-Elsevier
In this paper a fault accommodation approach especially suitable for nonlinear dynamic inversion controllers is presented and applied to an atmospheric re-entry vehicle. The approach is based on the nominal/robustness decoupling principle used in rec
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8b271d9b11d0bca9f3819f502dea8cba
https://doi.org/10.3182/20100906-5-jp-2022.00073
https://doi.org/10.3182/20100906-5-jp-2022.00073
Publikováno v:
IFAC Proceedings Volumes. 42:633-638
This paper presents the design process and evaluation of a fault detection and isolation (FDI) filter for the provision of health monitoring capabilities on the Hopper reusable launch vehicle (RLV) during a period of the re-entry. A high fidelity non
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a6eaab68be5a46d7c5773e121e339a45
https://doi.org/10.3182/20090630-4-es-2003.00105
https://doi.org/10.3182/20090630-4-es-2003.00105
Publikováno v:
IFAC Proceedings Volumes. 42:609-614
This paper presents results of an European Space Agency (ESA) study performed on health management for a re-usable launch vehicle (RLV). Though an overall system health management architecture is presented, focus is given to mission monitoring and GN
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bf7e4d0163cc3c07275d9e5d5a5ae157
https://doi.org/10.3182/20090630-4-es-2003.00101
https://doi.org/10.3182/20090630-4-es-2003.00101
Publikováno v:
IFAC Proceedings Volumes. 42:621-626
In this article the design of a fault tolerant thrust vector control (TVC) for the automated ascent of the Hopper reusable launch vehicle is presented. The considered ascent starts at the pull-up maneuver performed immediately after horizontal take o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a9b21ac0419fb02e5b26f4a526e80918
https://doi.org/10.3182/20090630-4-es-2003.00103
https://doi.org/10.3182/20090630-4-es-2003.00103
Publikováno v:
Acta Astronautica. 57:330-340
Separated space interferometers require performing different type of maneuvers during their lifetime: resizing, rotating and slewing. They shall be conducted within a given period while maintaining a constrained formation. Moreover, the maneuvers and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3a261d1e6b73213a649881c21d2fad29
https://doi.org/10.1016/j.actaastro.2005.03.025
https://doi.org/10.1016/j.actaastro.2005.03.025
Publikováno v:
Acta Astronautica. 55:495-507
When dealing with mission requirements calling for highly stable gravitational and thermal environments, one of the common options always considered is that of the heliocentric Earth trailing orbits (HETO). This is the case, for instance, of the Lase
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::db1927bbad4151f368b4f2d05df8808d
https://doi.org/10.1016/j.actaastro.2004.05.035
https://doi.org/10.1016/j.actaastro.2004.05.035
Autor:
David Orozco Suárez, Jose Carlos del Toro Iniesta, Francisco Javier Bailén Martínez, María Balaguer Jiménez, Daniel Álvarez García, Daniel Serrano, Luis F. Peñin, Alicia Vázquez-Ramos, Luis Ramón Bellot Rubio, Julia Atienzar, Isabel Pérez Grande, Ignacio Torralbo Gimeno, Esteban Sanchis Kilders, José Luis Gasent Blesa, David Hernández Expósito, Basilio Ruiz Cobo, Javier Trujillo Bueno, Robertus Erdélyi, Jackie A. Davies, Lucie M. Green, Sarah A. Matthews, David M. Long, Michail Mathioudakis, Christian Kintziger, Jorrit Leenaarts, Silvano Fineschi, Eamon Scullion
Publikováno v:
Aerospace, Vol 10, Iss 12, p 987 (2023)
Measuring magnetic fields in the inner corona, the interface between the solar chromosphere and outer corona, is of paramount importance if we aim to understand the energetic transformations taking place there, and because it is at the origin of proc
Externí odkaz:
https://doaj.org/article/4fd20ff3c6ab4bbfa6faaa95ffc655a8