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Design of spacecraft controller based on adaptive fuzzy sliding mode variable structure

  • Harbin Institute of Technology

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

Abstract

Using of feedback linearization technique to solve the problem of traditional sliding mode control chattering. The fuzzy adaptive control and sliding mode variable structure was designed by combining a novel adaptive fuzzy sliding mode variable structure controller. Through fuzzy inference and the stability analysis based on Lyapunov function to obtain fuzzy control rules adaptive law and effective solution to the traditional sliding mode control of the need to determine the parameter perturbation and external interference supremum uncertainty. Simulation results show that this method has better stability and robustness.

Original languageEnglish
Title of host publicationVehicle, Mechatronics and Information Technologies
Pages278-281
Number of pages4
DOIs
StatePublished - 2013
Event2013 International Conference on Vehicle and Mechanical Engineering and Information Technology, VMEIT 2013 - Zhengzhou, Henan, China
Duration: 17 Aug 201318 Aug 2013

Publication series

NameApplied Mechanics and Materials
Volume380-384
ISSN (Print)1660-9336
ISSN (Electronic)1662-7482

Conference

Conference2013 International Conference on Vehicle and Mechanical Engineering and Information Technology, VMEIT 2013
Country/TerritoryChina
CityZhengzhou, Henan
Period17/08/1318/08/13

Keywords

  • Fuzzy control
  • Linear feedback
  • Robustness
  • Sliding mode variable structure

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