Bordeneuve-Guibé, Joël and Dall'Orso, Mickael and Guy, Nicolas and Alazard, Daniel and Carpentier, Benjamin LPV techniques for the control of an airborne micro-launcher. (2011) In: 8th International ESA Conference on Guidance, Navigation & Control Systems - GNC 2011, 05-10 June 2011, Karlovy Vary, Czech Republic .
(Document in English)
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This paper addresses the robust control of a micro-launcher. The general framework of this work is a R&D project of the French space agency (CNES) focused on new launchers. The objective was to evaluate the potentialities of Linear Parameter Varying (LPV) techniques for the specific problem of launchers control. As a realistic test case, the micro-launcher preliminary research program, supported by the CNES Launcher Directorate, has been considered. First a Linear Fractional Transformation (LFT) based model of the launcher has been established and validated. Then two strategies have been chosen to design a robust controller of the angle of attack: a complete LPV controller has first been developed; then a controller based on an LFT representation of a classical lead phase controller has been considered. Realistic simulations have been conducted to compare both strategies with a more traditional interpolated lead phase controller. Finally, the simulation results exhibit very promising results, allowing a total respect of the performance specifications.
|Item Type:||Conference or Workshop Item (Paper)|
|Audience (conference):||International conference proceedings|
|Institution:||French research institutions > Centre National des Etudes Spatiales - CNES (FRANCE)|
Université de Toulouse > Institut Supérieur de l'Aéronautique et de l'Espace - ISAE (FRANCE)
French research institutions > Office National d'Etudes et Recherches Aérospatiales - ONERA (FRANCE)
Département de Mathématiques, Informatique, Automatique - DMIA (Toulouse, France) - Automatique, Dynamique et Interface des Systèmes - ADIS
|Deposited By:||joel bordeneuve-guibe|
|Deposited On:||25 Oct 2011 14:42|
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