Nonlinear H robust control for satellite large angle attitude maneuvers

研究成果: Conference article

13 引文 斯高帕斯(Scopus)

摘要

The paper presents a nonlinear H state feedback for large angle attitude control of satellite. The dynamic equations of satellite with full-coupled body fixed canted attitude thruster control are derived. A nonlinear H controller is designed to achieve stability and disturbance rejection for large angle maneuvers. The simulation results based on spacecraft system are presented to demonstrate the effectiveness of the proposed design method.

原文English
頁(從 - 到)1357-1362
頁數6
期刊Proceedings of the American Control Conference
2
出版狀態Published - 2001 一月 1
事件2001 American Control Conference - Arlington, VA, United States
持續時間: 2001 六月 252001 六月 27

    指紋

All Science Journal Classification (ASJC) codes

  • Electrical and Electronic Engineering

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