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Attitude maneuver control of flexible spacecraft with finite-time convergence

  • Shunan Wu*
  • , Zhaowei Sun
  • , Xiande Wu
  • *Corresponding author for this work
  • Harbin Institute of Technology
  • Harbin Engineering University

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

Abstract

The attitude maneuver control of flexible spacecraft with finite-time convergence is investigated in this paper. Two terminal sliding mode controllers are proposed to achieve the finite-time control, which guarantee the convergence of attitude maneuver errors in finite time. The singularity problem associated with the terminal sliding mode control is solved by employing a new sliding variable. Numerical simulations are finally provided to illustrate the performance of the proposed controllers.

Original languageEnglish
Title of host publicationMechatronics and Applied Mechanics
Pages847-851
Number of pages5
DOIs
StatePublished - 2012
EventMechatronics and Applied Mechanics - Hong Kong, Hong Kong
Duration: 27 Dec 201128 Dec 2011

Publication series

NameApplied Mechanics and Materials
Volume157-158
ISSN (Print)1660-9336
ISSN (Electronic)1662-7482

Conference

ConferenceMechatronics and Applied Mechanics
Country/TerritoryHong Kong
CityHong Kong
Period27/12/1128/12/11

Keywords

  • Attitude maneuver
  • Finite time
  • Flexible spacecraft
  • Terminal sliding mode control

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