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Legacy recovery and robust augmentation structured design for the VEGA launcher

Research output: Contribution to journalArticle

Original languageEnglish
Pages (from-to)3363-3388
Number of pages26
JournalInternational Journal of Robust and Nonlinear Control
Volume29
Issue number11
Early online date16 Apr 2019
DOIs
DateAccepted/In press - 21 Mar 2019
DateE-pub ahead of print - 16 Apr 2019
DatePublished (current) - 25 Jul 2019

Abstract

This paper presents a systematic robust control framework based on the structured H approach to address the synthesis of the atmospheric ascent-flight control system of a launch vehicle. To introduce this synthesis framework, the control problem is first formulated to recover the classically designed baseline rigid-body controller of the actual VEGA launcher VV05 mission. This legacy recovery builds the necessary background for a good understanding of the problem and increases confidence for its transfer to the Space industry. Subsequently, it is shown how to systematically augment the robustness of the design from the synthesis stage against wind turbulence perturbations and parametric uncertainty. The resulting controller is verified via classical stability margins and robust structured singular value analyses and finally validated using nonlinear, time-domain simulations in a Monte Carlo campaign. It is highlighted that this robust synthesis framework allows to obtain a controller with improved robust stability and global performance, and more importantly, it provides a more systematic methodology for design.

    Research areas

  • robust control synthesis, structured, VEGA launcher, μ analysis

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  • Full-text PDF (accepted author manuscript)

    Rights statement: This is the author accepted manuscript (AAM). The final published version (version of record) is available online via Wiley at https://onlinelibrary.wiley.com/doi/full/10.1002/rnc.4557 . Please refer to any applicable terms of use of the publisher.

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    Embargo ends: 16/04/20

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