Research on Sliding Mode Control of Folding-Wing Missile’s Lateral Overload

Yang Liang; Yang Jianying

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Research on Sliding Mode Control of Folding-Wing Missile’s Lateral Overload

Yang Liang * #,Yang Jianying

The State Key Laboratory for Turbulence and Complex Systems, College of Engineering, Peking University

*Correspondence author

#Submitted by

Subject:

Funding: 教育部重点基金（No.107110）

Opened online:23 February 2009

Accepted by: none

Citation: Yang Liang,Yang Jianying.Research on Sliding Mode Control of Folding-Wing Missile’s Lateral Overload[OL]. [23 February 2009] http://en.paper.edu.cn/en_releasepaper/content/29503

Considering that the folding-wing missile deploys its wings in short time, and such a transient but complicated process has a strong influence on its math model, we simplify the process into model\

Keywords:Folding wing；Lateral overload；Sliding mode control

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