The H∞ Reconfiguration Controller Design for Aircraft

Xiu Qin Yang; Xiao Jie Zhang; Kai Feng Zou

doi:10.4028/www.scientific.net/AMM.336-338.633

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 336-338The H∞ Reconfiguration Controller Design for...

The H_∞ Reconfiguration Controller Design for Aircraft

Abstract:

Base on the parameter of actuator failure the model of aircraft with failure is founded. After that a Hinf reconfiguration controller is designed with LMI to rescue for aircraft when some failure occurs at actuator. At the last the simulation is done about the Hinf reconfiguration controller figures how to work. And the figures about that is given.

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Periodical:

Applied Mechanics and Materials (Volumes 336-338)

Pages:

633-636

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.336-338.633

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Online since:

July 2013

Authors:

Xiu Qin Yang, Xiao Jie Zhang, Kai Feng Zou

Keywords:

Failure Parameter, Hinf Controller, LMI, Model

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