Researching variable structure control of moving mass reentry-vehicles

Peng Lin, Jun Zhou

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

7 Scopus citations

Abstract

This paper deals with the control of an axisymmetric moving mass actuated reentry vehicle. Three channel stable dynamic equations of the reentry vehicle are obtained derived from Newtonian theory. Since the maneuvering flighting in the reentry stage is mainly in the longitudinal plane, linear equations of the vehicle in the longitudinal plane based on linear perturbation theory are available. In addition, the control system of the moving mass actuated reentry vehicle is designed based on variable structure control method. Results obtained from simulations indicate the nonlinear model satisfy performance index demands of the attitude control.

Original languageEnglish
Title of host publicationProceedings - 2010 3rd IEEE International Conference on Computer Science and Information Technology, ICCSIT 2010
Pages126-129
Number of pages4
DOIs
StatePublished - 2010
Event2010 3rd IEEE International Conference on Computer Science and Information Technology, ICCSIT 2010 - Chengdu, China
Duration: 9 Jul 201011 Jul 2010

Publication series

NameProceedings - 2010 3rd IEEE International Conference on Computer Science and Information Technology, ICCSIT 2010
Volume8

Conference

Conference2010 3rd IEEE International Conference on Computer Science and Information Technology, ICCSIT 2010
Country/TerritoryChina
CityChengdu
Period9/07/1011/07/10

Keywords

  • Attitude control
  • Model-reference variable structure control
  • Moving mass control
  • Reentry vehicle

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