Electromagnetic satellite cluster collision prediction and avoidance

  • Jianmin Su*
  • , Yunfeng Dong
  • *Corresponding author for this work

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

Abstract

A two-spacecraft cluster in deep space collision prediction and avoidance is discussed in this paper, with double-integral model as dynamics model. Collision probability calculation is based on relative motion states and covariance matrix prediction. Collision avoidance mechanism, employing electromagnetic force as control force, distance and distance rate as feedback, will start when collision probability is beyond upper limit. Control law was designed by making use of Lyapunov method, aimed to avoid collision and make distance rate approach to zero.

Original languageEnglish
Title of host publicationProceedings - 2010 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2010
Pages767-770
Number of pages4
DOIs
StatePublished - 2010
Event2010 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2010 - Xiamen, China
Duration: 29 Oct 201031 Oct 2010

Publication series

NameProceedings - 2010 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2010
Volume2

Conference

Conference2010 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2010
Country/TerritoryChina
CityXiamen
Period29/10/1031/10/10

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