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Non-singular Terminal Sliding Mode Control for Fast Circumnavigate Mission Centered on Non-cooperative Spacecraft

  • Harbin Institute of Technology

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

Abstract

The problem of position and attitude 6-DOF coupling stabilization in the fast circumnavigate mission centered on a non-cooperative spacecraft with model uncertainties, external disturbances is investigated in this paper. First of all, a kinematics and dynamics model of active spacecraft in the circumnavigate mission is derived based on Newton's mechanics principle and quaternion theory. Then, the calculation method of desired quaternion is given, which can ensure continuous daylighting for active spacecraft. further, Based on the model mentioned above, an non-singular terminal sliding mode controller is proposed, which can force the tracking errors of relative quaternion and relative position coverge to zero in finite time. Finally, the effectiveness of the proposed controller is verified by numerical simulation.

Original languageEnglish
Title of host publicationProceedings - 2019 Chinese Automation Congress, CAC 2019
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages3658-3663
Number of pages6
ISBN (Electronic)9781728140940
DOIs
StatePublished - Nov 2019
Event2019 Chinese Automation Congress, CAC 2019 - Hangzhou, China
Duration: 22 Nov 201924 Nov 2019

Publication series

NameProceedings - 2019 Chinese Automation Congress, CAC 2019

Conference

Conference2019 Chinese Automation Congress, CAC 2019
Country/TerritoryChina
CityHangzhou
Period22/11/1924/11/19

Keywords

  • 6-DOF control
  • NTSM control.
  • dynamic couplings

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