Intelligent fuzzy variable structure control of flexible spacecraft

Yanan Yu*, Xiuyun Meng, Keyong Li

*Corresponding author for this work

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

Abstract

Aiming at the problem of vibration suppression of flexible spacecraft and high frequency chattering of sliding mode variable structure control torque, a real-time optimization sliding mode variable structure control algorithm based on the intelligent fuzzy method is proposed. Through designing variable structure control strategy with exponential approach law, the spacecraft attitude control and vibration suppression of flexible appendages are achieved. However, the control torque may present high frequency chattering during the sliding phase, and effect of vibration suppression will be weakened. The intelligent fuzzy control algorithm is used to eliminate chattering by optimizing parameters of the control system. Numerical simulations show that the high frequency chattering of control torque is restrained effectively and vibration suppression can be accomplished with faster convergence.

Original languageEnglish
Title of host publication2011 International Conference on Electrical and Control Engineering, ICECE 2011 - Proceedings
Pages4814-4817
Number of pages4
DOIs
Publication statusPublished - 2011
Event2nd Annual Conference on Electrical and Control Engineering, ICECE 2011 - Yichang, China
Duration: 16 Sept 201118 Sept 2011

Publication series

Name2011 International Conference on Electrical and Control Engineering, ICECE 2011 - Proceedings

Conference

Conference2nd Annual Conference on Electrical and Control Engineering, ICECE 2011
Country/TerritoryChina
CityYichang
Period16/09/1118/09/11

Keywords

  • fuzzy control
  • high frequency chattering
  • sliding mode control
  • vibration suppression

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