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Derivation and Analysis of a State-Space Model for Transient Control of Liquid-Propellant Rocket Engines

Sergio Pérez-Roca 1 Julien Marzat 1 Hélène Piet-Lahanier 1 Nicolas Langlois 2 Marco Galeotta 3 François Farago 4, 3 Serge Le Gonidec 5 
1 DTIS, ONERA, Université Paris Saclay (COmUE) [Palaiseau]
2 Pôle Automatique et Systèmes
IRSEEM - Institut de Recherche en Systèmes Electroniques Embarqués
3 CNES - Centre National d'Etudes Spatiales - Direction Des Lanceurs.
4 IMCCE - Institut de Mécanique Céleste et de Calcul des Ephémérides
5 ArianeGroup
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Conference papers
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https://hal-normandie-univ.archives-ouvertes.fr/hal-02282066
Contributor : Nicolas Langlois Connect in order to contact the contributor
Submitted on : Monday, September 9, 2019 - 4:45:44 PM
Last modification on : Wednesday, March 23, 2022 - 3:50:08 PM

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OBSPM | INSU | ONERA | CNRS | IMCCE | COMUE-NORMANDIE | TDS-MACS | PSL | UNIV-PARIS-SACLAY | IRSEEM | UNIROUEN | UNIV-LILLE | SORBONNE-UNIVERSITE | SU-SCIENCES | ESIGELEC | GS-ENGINEERING | GS-COMPUTER-SCIENCE

Citation

Sergio Pérez-Roca, Julien Marzat, Hélène Piet-Lahanier, Nicolas Langlois, Marco Galeotta, et al.. Derivation and Analysis of a State-Space Model for Transient Control of Liquid-Propellant Rocket Engines. 2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE), Jul 2018, Budapest, Hungary. pp.58-67, ⟨10.1109/icmae.2018.8467617⟩. ⟨hal-02282066⟩

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