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

Abstract : 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.
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Conference papers
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https://hal-supelec.archives-ouvertes.fr/hal-00826283
Contributor : Josiane Dartron <>
Submitted on : Monday, May 27, 2013 - 11:53:33 AM
Last modification on : Tuesday, August 27, 2019 - 11:54:03 AM

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  • HAL Id : hal-00826283, version 1

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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. ⟨hal-00826283⟩

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