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Variable structure control for tethered satellite fast deployment and retrieval

  • Northwestern Polytechnical University Xian

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

9 Scopus citations

Abstract

The control method for tethered satellite deployment and retrieval is important to meet its operation requirement. In this paper, dynamics model for a short tethered satellite system is established. The deployment and retrieval method for the short tethered satellite in fast operation is discussed. The sub-satellite could be developed with an initial velocity and decelerates in the deployment and retrieval period. Thrusters are used to control the direction of the tether. Variable structure control scheme is designed based on the dynamic character of the system and the output of the thrusters. Numerical simulation is carried out to test the efficiency of the control method. The tension of the tether is positive in both the development and retrieval period because of the acceleration of the tether. The Variable structure control system can keep the sub-satellite in designed direction. This control method can provide an idea for future tethered satellite control.

Original languageEnglish
Title of host publicationFuture Control and Automation - Proceedings of the 2nd International Conference on Future Control and Automation, ICFCA 2012
Pages157-164
Number of pages8
EditionVOL. 1
DOIs
StatePublished - 2012
Event3rd International Symposium on Artificial Intelligence, JSAI-isAI 2011 - Takamatsu, Japan
Duration: 1 Dec 20112 Nov 2012

Publication series

NameLecture Notes in Electrical Engineering
NumberVOL. 1
Volume172 LNEE
ISSN (Print)1876-1100
ISSN (Electronic)1876-1119

Conference

Conference3rd International Symposium on Artificial Intelligence, JSAI-isAI 2011
Country/TerritoryJapan
CityTakamatsu
Period1/12/112/11/12

Keywords

  • deployment
  • dynamics model
  • retrieval
  • tetherd satellite
  • variable structure control

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