Neuro-adaptive Distributed Finite-time Attitude Tracking Control for Multiple Rigid Spacecraft by Output Feedback

Bing Cui, Yuanqing Xia, Kun Liu, Ganghui Shen

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

Abstract

This paper is concerned with the distributed finite-time attitude tracking control problem for multiple uncertain rigid spacecraft in the presence of unavailable angular velocity under directed graph. First, a finite-time neuro-adaptive observer is proposed for each follower to estimate its own unavailable angular velocity. Then based on adding a power integrator technique, a distributed finite-time control scheme with only attitude measurements is developed. A rigorous theoretical proof shows that the finite-time stability of the overall closed-loop system is ensured. It is seen that the velocity-free control scheme is distributed and model-independent, resulting in an effective and low-cost strategy for spacecraft applications. A simulation with multiple spacecraft is given to verify the effectiveness of the proposed control scheme.

Original languageEnglish
Title of host publication3rd International Symposium on Autonomous Systems, ISAS 2019
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages266-271
Number of pages6
ISBN (Electronic)9781728112985
DOIs
Publication statusPublished - May 2019
Event3rd International Symposium on Autonomous Systems, ISAS 2019 - Shanghai, China
Duration: 29 May 201931 May 2019

Publication series

Name3rd International Symposium on Autonomous Systems, ISAS 2019

Conference

Conference3rd International Symposium on Autonomous Systems, ISAS 2019
Country/TerritoryChina
CityShanghai
Period29/05/1931/05/19

Keywords

  • Multiple rigid spacecraft
  • distributed attitude control
  • finite-time control

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