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Switching performance optimal controller design for hypersonic vehicle model

  • Yiwen Qi*
  • , Wen Bao
  • *Corresponding author for this work
  • Harbin Institute of Technology

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

This paper addresses the problem of switching performance optimal control for the longitudinal model of the generic hypersonic air-breathing flight vehicle. For the widening flight envelope of hypersonic vehicle, the multiple-mode switching control is an issue that have to be considered. The approach presented makes use of the bumpless transfer technique and gives a switching performance optimal controller design method for coping with bumps and undesirable transients in multiple-mode switching systems. Simulation results for the generic hypersonic vehicle model show the effectiveness of the proposed design method.

Original languageEnglish
Title of host publicationISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics
Pages137-142
Number of pages6
DOIs
StatePublished - 2010
Event3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010 - Harbin, China
Duration: 8 Jun 201010 Jun 2010

Publication series

NameISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics

Conference

Conference3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010
Country/TerritoryChina
CityHarbin
Period8/06/1010/06/10

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