Utilization of the bias momentum approach for capturing a tumbling satellite

Dimitar Nikolaev Dimitrov, Kazuya Yoshida

Research output: Chapter in Book/Report/Conference proceedingConference contribution

32 Citations (Scopus)

Abstract

This paper deals with problems related to the capture of a tumbling satellite by a space robot. The minimization of the base attitude deviation after the contact with the target is discussed from the viewpoint of angular momentum distribution. A new capturing strategy utilizing bias momentum is introduced. By using the null space of the coupling inertia matrix we present a method for angular momentum redistribution while following a desired trajectory.

Original languageEnglish
Title of host publication2004 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS)
Pages3333-3338
Number of pages6
Publication statusPublished - 2004 Dec 1
Event2004 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS) - Sendai, Japan
Duration: 2004 Sep 282004 Oct 2

Publication series

Name2004 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS)
Volume4

Other

Other2004 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS)
CountryJapan
CitySendai
Period04/9/2804/10/2

ASJC Scopus subject areas

  • Engineering(all)

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