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Dynamic obstacle avoidance of autonomous rendezvous and docking using potential function guidance based-fuzzy logic system

  • Dawei Zhang*
  • , Shenmin Song
  • , Run Pei
  • *Corresponding author for this work
  • School of Astronautics, Harbin Institute of Technology
  • Harbin Institute of Technology

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

Abstract

A guidance control method is proposed for the mission of autonomous rendezvous and docking with non-cooperative target spacecraft. Firstly, the relative motion equations of state are described in a line of sight coordinate frame. Then artificial potential function guidance based-fuzzy logic system, which adapts the parameters of the potential function, is used for chaser to approach non-cooperative target and avoid dynamic obstacles. Stability of the proposed method is analyzed by Lyapunov theory. Results obtained from numerical simulation studies demonstrate the validity of the method formulated in this paper.

Original languageEnglish
Title of host publicationISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics
Pages34-39
Number of pages6
DOIs
StatePublished - 2010
Event3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010 - Harbin, China
Duration: 8 Jun 201010 Jun 2010

Publication series

NameISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics

Conference

Conference3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010
Country/TerritoryChina
CityHarbin
Period8/06/1010/06/10

Keywords

  • Artificial potential function guidance
  • Autonomous rendezvous and docking
  • Dynamic obstacle avoidance
  • Fuzzy logic system
  • Non-cooperative target

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