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A Non-singular Terminal Sliding Mode Attitude Control for Space Robots

  • Yiwei Tang
  • , Yingmin Jia*
  • *Corresponding author for this work
  • Beihang University

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

Abstract

In this paper, a non-singular terminal sliding mode method is proposed for attitude tracking of space robots, which makes base attitudes and joint angles of space robots to track the desired trajectories in finite time under external disturbances and uncertain parameters. Finally, the effectiveness of the control method is verified by SolidWork and Simulink.

Original languageEnglish
Title of host publicationProceedings of 2022 Chinese Intelligent Systems Conference - Volume II
EditorsYingmin Jia, Weicun Zhang, Yongling Fu, Shoujun Zhao
PublisherSpringer Science and Business Media Deutschland GmbH
Pages1-8
Number of pages8
ISBN (Print)9789811962257
DOIs
StatePublished - 2022
Event18th Chinese Intelligent Systems Conference, CISC 2022 - Beijing, China
Duration: 15 Oct 202216 Oct 2022

Publication series

NameLecture Notes in Electrical Engineering
Volume951 LNEE
ISSN (Print)1876-1100
ISSN (Electronic)1876-1119

Conference

Conference18th Chinese Intelligent Systems Conference, CISC 2022
Country/TerritoryChina
CityBeijing
Period15/10/2216/10/22

Keywords

  • Attitude tracking
  • Finite-time control
  • Non-singular terminal sliding mode
  • Space robots

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