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Self-regulation control scheme for reusable launch vehicle reentry attitude control

  • Jianshuang Song*
  • , Zhang Ren
  • , Zhen Shen
  • *Corresponding author for this work
  • Beihang University
  • Civil Aviation Management Institute of China

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

Abstract

Integrating sliding mode control and nonlinear dynamic inversion technique forms a new robust controller. Using nonlinear extended state observer to build the estimation of system disturbance, and based on the estimation, magnitude of the sliding mode item could be regulated to improve the control effect. Stability of This new controller is analyzed. This new control scheme is used in the reentry attitude control for reusable launch vehicle. Feasibility and validity of the new controller is demonstrated with simulation examples.

Original languageEnglish
Title of host publication2012 IEEE 5th International Conference on Advanced Computational Intelligence, ICACI 2012
Pages447-451
Number of pages5
DOIs
StatePublished - 2012
Event2012 IEEE 5th International Conference on Advanced Computational Intelligence, ICACI 2012 - Nanjing, China
Duration: 18 Oct 201220 Oct 2012

Publication series

Name2012 IEEE 5th International Conference on Advanced Computational Intelligence, ICACI 2012

Conference

Conference2012 IEEE 5th International Conference on Advanced Computational Intelligence, ICACI 2012
Country/TerritoryChina
CityNanjing
Period18/10/1220/10/12

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