Prescribed Perfomance Finite-Time Attitude Tracking Control of Spinning Tether System base on Backstepping Method

Yi Chen, Changqing Wang, Aijun Li, Hao Chang Tian, Ying Zhang

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

Abstract

This paper mainly focuses on the attitude control of end-body spacecraft during the rotation of spinning tether system (STS). First, the Newton-Euler method is used to establish the kinematics and attitude dynamics models of the spinning tether system. Based on the quaternion theory, the attitude kinematics equations of the tether system described by quaternion are derived, and the closed-loop attitude tracking error model is derived accordingly. Then, a new finite-time performance function (FTPF) is used to design a prescribed performance finite-time attitude controller based on back-stepping method. This controller can make the attitude tracking error converge to the expected region in finite time. Finally, the effectiveness of the proposed method is verified by numerical simulation.

Original languageEnglish
Title of host publicationProceeding - 2021 China Automation Congress, CAC 2021
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages6850-6855
Number of pages6
ISBN (Electronic)9781665426473
DOIs
StatePublished - 2021
Event2021 China Automation Congress, CAC 2021 - Beijing, China
Duration: 22 Oct 202124 Oct 2021

Publication series

NameProceeding - 2021 China Automation Congress, CAC 2021

Conference

Conference2021 China Automation Congress, CAC 2021
Country/TerritoryChina
CityBeijing
Period22/10/2124/10/21

Keywords

  • attitude control
  • Finite-time boundedness
  • prescribed performance control
  • spinning tether system

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