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
3 CNES - Centre National d'Etudes Spatiales - Direction Des Lanceurs.
4 IMCCE - Institut de Mécanique Céleste et de Calcul des Ephémérides
5 ArianeGroup

Domains: Engineering Sciences [physics]; Automatic

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⟩