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Finite-time attitude consensus tracking with terminal sliding mode observer

  • Harbin Institute of Technology Weihai

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

Abstract

In this paper, a distributed attitude consensus tracking control law is proposed for satellite formation flying by using sliding mode method. First, graph theory and Modified Rodriguez Parameters (MRPs) are introduced to describe the relation and dynamics of the team. Second, distributed terminal sliding mode observers are constructed to estimate the velocity state of rigid bodies in the team. The observer error will converge to zero in finite time. Then, an attitude consensus tracking control law based on sliding mode method is discussed, using the estimated states by the proposed observers. The control law can ensure not only attitude agreement between rigid bodies in the team but also time-varying reference tracking without velocity measurements. Finally, an illustrative example shows that the attitude tracking goal will achieve with the velocity-free consensus control strategy.

Original languageEnglish
Title of host publication26th Chinese Control and Decision Conference, CCDC 2014
PublisherIEEE Computer Society
Pages1141-1146
Number of pages6
ISBN (Print)9781479937066
DOIs
StatePublished - 2014
Externally publishedYes
Event26th Chinese Control and Decision Conference, CCDC 2014 - Changsha, China
Duration: 31 May 20142 Jun 2014

Publication series

Name26th Chinese Control and Decision Conference, CCDC 2014

Conference

Conference26th Chinese Control and Decision Conference, CCDC 2014
Country/TerritoryChina
CityChangsha
Period31/05/142/06/14

Keywords

  • attitude tracking
  • finite-time consensus
  • sliding mode method
  • velocity-free

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