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Prescribed performance based finite-time attitude tracking control for rigid spacecraft

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

Abstract

This paper investigates the attitude tracking control problem for rigid spacecraft with bounded external disturbance. By combing the terminal sliding-mode technique and the prescribed performance concept, a finite-time control scheme with sliding-mode surface constraint is proposed, whose structure is simpler than the conventional transformed error constraint methods. Then, a saturation function is introduced to the control scheme to eliminate singularity, and the system performance in both the reaching phase and the ideal sliding-mode are studied. Stability analysis shows that the proposed control scheme can make the spacecraft tracking a time-varying desired signal with a finite-time convergence. The effectiveness of the attitude tracking control scheme is evaluated by numerical simulations.

Original languageEnglish
Title of host publication8th International Conference on Information Science and Technology, ICIST 2018
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages121-126
Number of pages6
ISBN (Print)9781538637814
DOIs
StatePublished - 6 Aug 2018
Event8th International Conference on Information Science and Technology, ICIST 2018 - Cordoba, Granada, and Seville, Spain
Duration: 30 Jun 20186 Jul 2018

Publication series

Name8th International Conference on Information Science and Technology, ICIST 2018

Conference

Conference8th International Conference on Information Science and Technology, ICIST 2018
Country/TerritorySpain
CityCordoba, Granada, and Seville
Period30/06/186/07/18

Keywords

  • prescribed performance control
  • spacecraft attitude tracking
  • terminal sliding-mode approach

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