Structured H-Infinity Control Based on Classical Control Parameters for the VEGA Launch Vehicle

Diego Navarro-Tapia, Andres Marcos, Samir Bennani, Christophe Roux

Research output: Chapter in Book/Report/Conference proceedingConference Contribution (Conference Proceeding)

4 Citations (Scopus)
273 Downloads (Pure)

Abstract

This article describes a methodology for structured H-infinity synthesis that reconciles classical and robust control concepts. The aim is to provide a transparent and methodological process to tune the weights used in the structured synthesis. The process is exemplified on a simplified model for the atmospheric ascent-flight control system for the VEGA launch vehicle. The results show that the same gains used for a real flight can be recovered leading the path for industrial transfer of the H-infinity structured control to launchers.
Original languageEnglish
Title of host publication2016 IEEE Conference on Control Applications (CCA 2016)
Subtitle of host publicationProceedings of a meeting held 19-22 September 2016, Buenos Aires, Argentina
Place of PublicationBuenos Aires, Argentina
PublisherInstitute of Electrical and Electronics Engineers (IEEE)
Pages33-38
Number of pages6
ISBN (Electronic)9781509007554
ISBN (Print)9781509007561
DOIs
Publication statusPublished - Nov 2016
Event2016 IEEE Conference on Control Applications (CCA) - Buenos Aires, Argentina
Duration: 19 Sep 201622 Sep 2016
http://ieeexplore.ieee.org/xpl/mostRecentIssue.jsp?punumber=7581720

Conference

Conference2016 IEEE Conference on Control Applications (CCA)
CountryArgentina
CityBuenos Aires
Period19/09/1622/09/16
Internet address

Keywords

  • robust control
  • aerospace control
  • Structured H-infinity synthesis

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