Adaptive sliding mode control for uncertain airplane control systems based on higher-order differential sliding mode surface

Airplane control system is a typical multitude input and multitude output (MIMO) nonlinear system with strong coupling and uncertainties, which would increase the controlling difficulty. The tracking control problem has been investigated for a class of airplane attitude control systems in this paper...

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Bibliographic Details
Main Authors: Xiaojing WU, Xueli WU, Shikai SHAO, Huixian LIU
Format: Article
Language:zho
Published: Hebei University of Science and Technology 2018-10-01
Series:Journal of Hebei University of Science and Technology
Subjects:
Online Access:http://xuebao.hebust.edu.cn/hbkjdx/ch/reader/create_pdf.aspx?file_no=b201805008&flag=1&journal_