Dynamics modeling and comparative robust stability analysis of a space launcher with constrained inputs - CentraleSupélec
Communication Dans Un Congrès Année : 2013

Dynamics modeling and comparative robust stability analysis of a space launcher with constrained inputs

Résumé

This paper presents a comparative robust stability analysis using IQC-based and LMI-based tools. An LFR, resulting from the factorization of the equations of motion, allows assessing the robust stability of a space launcher in the face of inertia uncertainties and saturated inputs.

Domaines

Sciences de l'ingénieur [physics]

Josiane Dartron  : Connectez-vous pour contacter le contributeur

https://centralesupelec.hal.science/hal-00826283

Soumis le : lundi 27 mai 2013-11:53:33

Dernière modification le : jeudi 28 novembre 2024-15:08:02

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Dates et versions

hal-00826283 , version 1 (27-05-2013)

Identifiants

Citer

Julien Chaudenson, Dominique Beauvois, S. Bennani, M. Ganet-Schoeller, Guillaume Sandou. Dynamics modeling and comparative robust stability analysis of a space launcher with constrained inputs. 12th European Control Conference (ECC 2013), Jul 2013, Zurich, Switzerland. pp.353-358, ⟨10.23919/ecc.2013.6669716⟩. ⟨hal-00826283⟩

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