LPV-Based Self-Adaption Integral Sliding Mode Controller With <inline-formula> <tex-math notation="LaTeX">$L_{2}$ </tex-math></inline-formula> Gain Performance for a Morphing Aircraft

LPV-Based Self-Adaption Integral Sliding Mode Controller With <inline-formula> <tex-math notation="LaTeX">$L_{2}$ </tex-math></inline-formula> Gain Performance for a Morphing Aircraft

This paper designs a parameter-dependent self-adaption integral sliding mode controller which converges the system in a finite time while focusing on an uncertain linear parameter varying (LPV) model of a variant aircraft that has a large-scale variation of the sweep angle and an extension. This des...

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Bibliographic Details
Main Authors: Qian Wu, Zhenghua Liu, Fanning Liu, Xuekun Chen
Format: Article
Language:English
Published: IEEE 2019-01-01
Series:IEEE Access
Subjects:
Morphing Aircraft
robust control
LPV
integral sliding mode
adaptive control
Online Access:https://ieeexplore.ieee.org/document/8737685/

Internet

https://ieeexplore.ieee.org/document/8737685/

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