Design of LPV-Based Sliding Mode Controller with Finite Time Convergence for a Morphing Aircraft

Design of LPV-Based Sliding Mode Controller with Finite Time Convergence for a Morphing Aircraft

This paper proposes a finite time convergence sliding mode control (FSMC) strategy based on linear parameter-varying (LPV) methodology for the stability control of a morphing aircraft subject to parameter uncertainties and external disturbances. Based on the Kane method, a longitudinal dynamic model...

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Bibliographic Details
Main Authors:	Nuan Wen, Zhenghua Liu, Yang Sun, Lingpu Zhu
Format:	Article
Language:	English
Published:	Hindawi Limited 2017-01-01
Series:	International Journal of Aerospace Engineering
Online Access:	http://dx.doi.org/10.1155/2017/8426348

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