Spacecraft robust attitude control attitude control with saturation nonlinearity

Long Life Show, Jyh Ching Juang, Ying Wen Jan, Chen Tsung Lin

研究成果: Conference contribution

4 引文 斯高帕斯(Scopus)

摘要

The paper presents a robust nonlinear H control design method for rigid spacecraft asymptotic attitude control with input saturation nonlinearity. The solution of the nonlinear H control problem is known to related to the existence of solution to a Hamilton-Jacobi partially differential inequality (HJPDI). The papers proposes a candidate solution to the HJPDI for spacecraft attitude control that is subject to nonlinear dynamics and input saturation. The method is applied to the ROCSAT-3 attitude control problem to verify its effectiveness.

原文English
主出版物標題AIAA Guidance, Navigation, and Control Conference and Exhibit
發行者American Institute of Aeronautics and Astronautics Inc.
ISBN(列印)9781624101083
出版狀態Published - 2002 1月 1
事件AIAA Guidance, Navigation, and Control Conference and Exhibit 2002 - Monterey, CA, United States
持續時間: 2002 8月 52002 8月 8

出版系列

名字AIAA Guidance, Navigation, and Control Conference and Exhibit

Other

OtherAIAA Guidance, Navigation, and Control Conference and Exhibit 2002
國家/地區United States
城市Monterey, CA
期間02-08-0502-08-08

All Science Journal Classification (ASJC) codes

  • 航空工程
  • 控制與系統工程
  • 電氣與電子工程

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