Position and attitude feedback controller of a planar satellite with two thrusters

Takashi Matsuno, Shinji Hokamoto

研究成果: Chapter in Book/Report/Conference proceedingConference contribution

2 被引用数 (Scopus)

抄録

This paper proposes a feedback control method for the in-plane motion of a satellite equipped with two thrusters, whose force directions are fixed to the satellite. The satellite's equations of motion have second-order nonholonomic constraints. This paper utilizes an invariant manifold and develops a feedback controller based on the Lyapunov's second method. The developed controller can control the satellite's state composed of six components for the position and attitude angle by two thruster systems. Furthermore, the controller has robustness for the system's modeling errors. Some simulations results are shown to demonstrate the effectiveness of the developed controller.

本文言語英語
ホスト出版物のタイトルICCAS-SICE 2009 - ICROS-SICE International Joint Conference 2009, Proceedings
ページ4206-4211
ページ数6
出版ステータス出版済み - 12 1 2009
イベントICROS-SICE International Joint Conference 2009, ICCAS-SICE 2009 - Fukuoka, 日本
継続期間: 8 18 20098 21 2009

出版物シリーズ

名前ICCAS-SICE 2009 - ICROS-SICE International Joint Conference 2009, Proceedings

その他

その他ICROS-SICE International Joint Conference 2009, ICCAS-SICE 2009
Country日本
CityFukuoka
Period8/18/098/21/09

All Science Journal Classification (ASJC) codes

  • Information Systems
  • Control and Systems Engineering
  • Industrial and Manufacturing Engineering

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