Nonlinear H robust control for satellite large angle attitude maneuvers

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13 Citations (Scopus)


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.

Original languageEnglish
Pages (from-to)1357-1362
Number of pages6
JournalProceedings of the American Control Conference
Publication statusPublished - 2001 Jan 1
Event2001 American Control Conference - Arlington, VA, United States
Duration: 2001 Jun 252001 Jun 27

All Science Journal Classification (ASJC) codes

  • Electrical and Electronic Engineering


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