Cooperation attitude control of multiple spacecraft using sliding mode variable structure

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Abstract

This paper focuses on the attitude control for multiple spacecraft. Two decentralized finite-time control laws are proposed when the communication topologies are directed and undirected, respectively. The proposed control schemes rely on the information of angular velocity errors and error quaternions of the neighboring spacecraft which determines the orientation of the torques and reduce the relative errors. Finite-time stabilization of the system is proved by using Lyapunov function and graph theory. Finally, simulation examples are illustrated to validate the approach by different case studies.

Original languageEnglish
Title of host publicationProceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages1828-1833
Number of pages6
ISBN (Electronic)9781479925384
DOIs
Publication statusPublished - 31 Aug 2015
EventInternational Conference on Mechatronics and Control, ICMC 2014 - Jinzhou, China
Duration: 3 Jul 20145 Jul 2014

Publication series

NameProceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014

Conference

ConferenceInternational Conference on Mechatronics and Control, ICMC 2014
Country/TerritoryChina
CityJinzhou
Period3/07/145/07/14

Keywords

  • Angular velocity
  • Attitude control
  • Laplace equations
  • Quaternions
  • Space vehicles
  • Synchronization
  • Topology

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