Design procedure of chattering attenuation sliding mode attitude control of a satellite system

Hamidreza Nemati, Shinji Hokamoto

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

2 被引用数 (Scopus)

抄録

This study presents a design procedure for a new robust nonlinear control algorithm based on the theory of the terminal sliding mode (TSM) to control the attitude of a satellite system. Since the traditional TSM controllers include a discontinuous function, a significant problem called chattering can occur. In this paper, a methodology for designing a new switching function is discussed to alleviate this drawback over time. Besides, to highlight the robustness of the proposed method against uncertainties, a satellite with three pairs of thrusters subject to parameter variation is simulated.

本文言語英語
ホスト出版物のタイトルAdvances In The Astronautical Sciences
出版社Univelt Inc.
ページ3533-3541
ページ数9
152
ISBN(電子版)9780877036111
出版ステータス出版済み - 2014
イベント24th AAS/AIAA Space Flight Mechanics Meeting, 2014 - Mexico, 米国
継続期間: 1 26 20141 30 2014

その他

その他24th AAS/AIAA Space Flight Mechanics Meeting, 2014
Country米国
CityMexico
Period1/26/141/30/14

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

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