Nonlinear H∞ robust control for satellite large angle attitude maneuvers

L. L. Show; Jyh-Chin Juang; Ciann-Dong Yang

Nonlinear H_∞ robust control for satellite large angle attitude maneuvers

L. L. Show, Jyh-Chin Juang, Ciann-Dong Yang

Research output: Contribution to journal › Conference article › peer-review

Abstract

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 language	English
Pages (from-to)	1357-1362
Number of pages	6
Journal	Proceedings of the American Control Conference
Volume	2
Publication status	Published - 2001 Jan 1
Event	2001 American Control Conference - Arlington, VA, United States Duration: 2001 Jun 25 → 2001 Jun 27

All Science Journal Classification (ASJC) codes

Electrical and Electronic Engineering

Cite this

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title = "Nonlinear H∞ robust control for satellite large angle attitude maneuvers",

abstract = "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.",

author = "Show, {L. L.} and Jyh-Chin Juang and Ciann-Dong Yang",

year = "2001",

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AU - Show, L. L.

AU - Juang, Jyh-Chin

AU - Yang, Ciann-Dong

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Y1 - 2001/1/1

N2 - 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.

AB - 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.

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M3 - Conference article

AN - SCOPUS:0034857723

SN - 0743-1619

VL - 2

SP - 1357

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JO - Proceedings of the American Control Conference

JF - Proceedings of the American Control Conference

T2 - 2001 American Control Conference

Y2 - 25 June 2001 through 27 June 2001

ER -

Nonlinear H_∞ robust control for satellite large angle attitude maneuvers

Abstract

All Science Journal Classification (ASJC) codes

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