A Control Method of Hypersonic Vehicle Based on the Structured Singular Value Theory

Gang Li; Lin Wei Xu; Hao He; Xing An

doi:10.4028/www.scientific.net/AMM.128-129.761

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 128-129A Control Method of Hypersonic Vehicle Based on...

A Control Method of Hypersonic Vehicle Based on the Structured Singular Value Theory

Abstract:

Firstly, the conception of hypersonic flight and its flight characteristics are introduced in the article. Secondly, a control method based on the structured singular value theory is proposed, and the necessity of this method whether can be applied to design the hypersonic vehicle controller is discussed. And then taking a model for example, the robust controller of hypersonic vehicle is designed. At last, the control effect of this controller is proved better through the simulation result. It also turned out that the controller has excellent command track performance.

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Periodical:

Applied Mechanics and Materials (Volumes 128-129)

Pages:

761-764

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.128-129.761

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Online since:

October 2011

Authors:

Gang Li, Lin Wei Xu, Hao He, Xing An

Keywords:

Hypersonic, Model, Robust Control, μ Analysis, μ-Synthesis

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